View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68811U 26145.30354985 +.00000000 +00000-0 +14236-2 0 00000
2 68811 97.2852 351.9633 0002025 76.7195 283.4296 15.75213445 04
| Epoch (UTC): | 25 May 2026 07:17:06 |
| Eccentricity: | 0.0002025 |
| inclination: | 97.2852° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9633° |
| argument of perigee: | 76.7195° |
| revolutions per day: | 15.75213445 |
| mean anomaly at epoch: | 283.4296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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